Blériot-SPAD S.XXIV
| S.XXIV | |
|---|---|
| Role | Fighter |
| National origin | France |
| Manufacturer | Blériot |
| Designer | André Herbemont |
| First flight | 5 November 1918 |
| Number built | 1 |
The SPAD S.XXIV was a prototype fighter plane built by SPAD at the end of World War I.
Design and development[edit]
The S.XXIV was a single-seat biplane fighter of all-wood construction with a canvas coating and a monocoque fuselage.
Specifications (variant specified)[edit]
Data from [1]
General characteristics
- Crew: 1
- Length: 6.48 m (21 ft 3 in)
- Wingspan: 9.8 m (32 ft 2 in)
- Height: 2.56 m (8 ft 5 in)
- Wing area: 26.2 m2 (282 sq ft)
- Empty weight: 650 kg (1,433 lb)
- Powerplant: 1 × Hispano-Suiza 8Bc V-8 wat3er-cooled piston engine, 160 kW (220 hp)
Performance
References[edit]
- ^ "SPAD S-XXIV - SPAD 24 - Chasseur - Un siècle d'aviation française". Aviafrance.com. 2002-12-14. Retrieved 2019-02-04.